EP3022024A2 - Nanocomposite vessels - Google Patents
Nanocomposite vesselsInfo
- Publication number
- EP3022024A2 EP3022024A2 EP14826218.1A EP14826218A EP3022024A2 EP 3022024 A2 EP3022024 A2 EP 3022024A2 EP 14826218 A EP14826218 A EP 14826218A EP 3022024 A2 EP3022024 A2 EP 3022024A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- vessel
- nanocomposite
- seamless
- functionalized
- epoxy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 239000002114 nanocomposite Substances 0.000 title claims abstract description 94
- 229920000642 polymer Polymers 0.000 claims abstract description 46
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 40
- 239000000463 material Substances 0.000 claims abstract description 25
- 229910052751 metal Inorganic materials 0.000 claims abstract description 16
- 239000002184 metal Substances 0.000 claims abstract description 16
- 238000000034 method Methods 0.000 claims abstract description 12
- 239000012815 thermoplastic material Substances 0.000 claims abstract description 8
- 239000010410 layer Substances 0.000 claims description 70
- 239000004593 Epoxy Substances 0.000 claims description 56
- 230000004888 barrier function Effects 0.000 claims description 44
- 239000011248 coating agent Substances 0.000 claims description 40
- 238000000576 coating method Methods 0.000 claims description 40
- 229920005989 resin Polymers 0.000 claims description 40
- 239000011347 resin Substances 0.000 claims description 40
- 239000002828 fuel tank Substances 0.000 claims description 24
- 229930195733 hydrocarbon Natural products 0.000 claims description 24
- 150000002430 hydrocarbons Chemical class 0.000 claims description 24
- 229920001903 high density polyethylene Polymers 0.000 claims description 22
- 239000004700 high-density polyethylene Substances 0.000 claims description 22
- 239000000835 fiber Substances 0.000 claims description 19
- 239000007789 gas Substances 0.000 claims description 18
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 17
- 229910052760 oxygen Inorganic materials 0.000 claims description 17
- 239000001301 oxygen Substances 0.000 claims description 17
- 239000000945 filler Substances 0.000 claims description 15
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 15
- 238000003860 storage Methods 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 13
- 239000003795 chemical substances by application Substances 0.000 claims description 11
- 239000006260 foam Substances 0.000 claims description 10
- 239000006229 carbon black Substances 0.000 claims description 8
- 230000035699 permeability Effects 0.000 claims description 8
- 239000004215 Carbon black (E152) Substances 0.000 claims description 7
- 239000002657 fibrous material Substances 0.000 claims description 6
- 239000003345 natural gas Substances 0.000 claims description 6
- 239000002344 surface layer Substances 0.000 claims description 6
- -1 polypropylene Polymers 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 4
- 239000012802 nanoclay Substances 0.000 claims description 4
- GNFTZDOKVXKIBK-UHFFFAOYSA-N 3-(2-methoxyethoxy)benzohydrazide Chemical compound COCCOC1=CC=CC(C(=O)NN)=C1 GNFTZDOKVXKIBK-UHFFFAOYSA-N 0.000 claims description 3
- 241000234282 Allium Species 0.000 claims description 3
- 235000002732 Allium cepa var. cepa Nutrition 0.000 claims description 3
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 claims description 3
- XMWRBQBLMFGWIX-UHFFFAOYSA-N C60 fullerene Chemical class C12=C3C(C4=C56)=C7C8=C5C5=C9C%10=C6C6=C4C1=C1C4=C6C6=C%10C%10=C9C9=C%11C5=C8C5=C8C7=C3C3=C7C2=C1C1=C2C4=C6C4=C%10C6=C9C9=C%11C5=C5C8=C3C3=C7C1=C1C2=C4C6=C2C9=C5C3=C12 XMWRBQBLMFGWIX-UHFFFAOYSA-N 0.000 claims description 3
- 239000004952 Polyamide Substances 0.000 claims description 3
- 229910021393 carbon nanotube Inorganic materials 0.000 claims description 3
- 239000002041 carbon nanotube Substances 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 229910003472 fullerene Inorganic materials 0.000 claims description 3
- 229910021389 graphene Inorganic materials 0.000 claims description 3
- 229910002804 graphite Inorganic materials 0.000 claims description 3
- 239000010439 graphite Substances 0.000 claims description 3
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 229920002647 polyamide Polymers 0.000 claims description 3
- 230000002787 reinforcement Effects 0.000 claims description 3
- 238000004544 sputter deposition Methods 0.000 claims description 3
- 229920001567 vinyl ester resin Polymers 0.000 claims description 3
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 claims description 2
- 239000004962 Polyamide-imide Substances 0.000 claims description 2
- 239000004743 Polypropylene Substances 0.000 claims description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 claims description 2
- 229920002312 polyamide-imide Polymers 0.000 claims description 2
- 229920001748 polybutylene Polymers 0.000 claims description 2
- 229920000306 polymethylpentene Polymers 0.000 claims description 2
- 239000011116 polymethylpentene Substances 0.000 claims description 2
- 229920001155 polypropylene Polymers 0.000 claims description 2
- 239000004927 clay Substances 0.000 description 15
- 229910001428 transition metal ion Inorganic materials 0.000 description 12
- 239000000446 fuel Substances 0.000 description 11
- 239000002105 nanoparticle Substances 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000013461 design Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 6
- 239000004917 carbon fiber Substances 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 229920000049 Carbon (fiber) Polymers 0.000 description 4
- 229940123973 Oxygen scavenger Drugs 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 239000002131 composite material Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000011258 core-shell material Substances 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 229920001169 thermoplastic Polymers 0.000 description 4
- 239000004416 thermosoftening plastic Substances 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 150000001768 cations Chemical class 0.000 description 3
- 239000002734 clay mineral Substances 0.000 description 3
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 239000006185 dispersion Substances 0.000 description 3
- 239000011152 fibreglass Substances 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- 239000004698 Polyethylene Substances 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 2
- 239000012790 adhesive layer Substances 0.000 description 2
- 238000000071 blow moulding Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 229920006334 epoxy coating Polymers 0.000 description 2
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 2
- 239000011229 interlayer Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 239000002516 radical scavenger Substances 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000002000 scavenging effect Effects 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 150000003623 transition metal compounds Chemical class 0.000 description 2
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical group [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- FOIXSVOLVBLSDH-UHFFFAOYSA-N Silver ion Chemical compound [Ag+] FOIXSVOLVBLSDH-UHFFFAOYSA-N 0.000 description 1
- YKTSYUJCYHOUJP-UHFFFAOYSA-N [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] Chemical compound [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] YKTSYUJCYHOUJP-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- KCZFLPPCFOHPNI-UHFFFAOYSA-N alumane;iron Chemical compound [AlH3].[Fe] KCZFLPPCFOHPNI-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- HPTYUNKZVDYXLP-UHFFFAOYSA-N aluminum;trihydroxy(trihydroxysilyloxy)silane;hydrate Chemical compound O.[Al].[Al].O[Si](O)(O)O[Si](O)(O)O HPTYUNKZVDYXLP-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000000440 bentonite Substances 0.000 description 1
- 229910000278 bentonite Inorganic materials 0.000 description 1
- SVPXDRXYRYOSEX-UHFFFAOYSA-N bentoquatam Chemical compound O.O=[Si]=O.O=[Al]O[Al]=O SVPXDRXYRYOSEX-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000001506 calcium phosphate Substances 0.000 description 1
- 229910000389 calcium phosphate Inorganic materials 0.000 description 1
- 235000011010 calcium phosphates Nutrition 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 229910000420 cerium oxide Inorganic materials 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000002860 competitive effect Effects 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229920001577 copolymer Polymers 0.000 description 1
- GUJOJGAPFQRJSV-UHFFFAOYSA-N dialuminum;dioxosilane;oxygen(2-);hydrate Chemical compound O.[O-2].[O-2].[O-2].[Al+3].[Al+3].O=[Si]=O.O=[Si]=O.O=[Si]=O.O=[Si]=O GUJOJGAPFQRJSV-UHFFFAOYSA-N 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 238000004299 exfoliation Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000003063 flame retardant Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 125000000524 functional group Chemical group 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 229910052621 halloysite Inorganic materials 0.000 description 1
- 229910000271 hectorite Inorganic materials 0.000 description 1
- KWLMIXQRALPRBC-UHFFFAOYSA-L hectorite Chemical compound [Li+].[OH-].[OH-].[Na+].[Mg+2].O1[Si]2([O-])O[Si]1([O-])O[Si]([O-])(O1)O[Si]1([O-])O2 KWLMIXQRALPRBC-UHFFFAOYSA-L 0.000 description 1
- 238000005984 hydrogenation reaction Methods 0.000 description 1
- 238000006459 hydrosilylation reaction Methods 0.000 description 1
- 230000002706 hydrostatic effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- NLYAJNPCOHFWQQ-UHFFFAOYSA-N kaolin Chemical compound O.O.O=[Al]O[Si](=O)O[Si](=O)O[Al]=O NLYAJNPCOHFWQQ-UHFFFAOYSA-N 0.000 description 1
- 229910052622 kaolinite Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 229910052901 montmorillonite Inorganic materials 0.000 description 1
- 239000011185 multilayer composite material Substances 0.000 description 1
- 239000002055 nanoplate Substances 0.000 description 1
- 239000002071 nanotube Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 150000002892 organic cations Chemical class 0.000 description 1
- BMMGVYCKOGBVEV-UHFFFAOYSA-N oxo(oxoceriooxy)cerium Chemical compound [Ce]=O.O=[Ce]=O BMMGVYCKOGBVEV-UHFFFAOYSA-N 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 238000009931 pascalization Methods 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 238000005191 phase separation Methods 0.000 description 1
- 239000010452 phosphate Substances 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000002952 polymeric resin Substances 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000012779 reinforcing material Substances 0.000 description 1
- 230000001846 repelling effect Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- 229910021647 smectite Inorganic materials 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000006277 sulfonation reaction Methods 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- QORWJWZARLRLPR-UHFFFAOYSA-H tricalcium bis(phosphate) Chemical compound [Ca+2].[Ca+2].[Ca+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O QORWJWZARLRLPR-UHFFFAOYSA-H 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000011787 zinc oxide Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K15/03006—Gas tanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K15/03177—Fuel tanks made of non-metallic material, e.g. plastics, or of a combination of non-metallic and metallic material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/02—Coating on the layer surface on fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/306—Resistant to heat
- B32B2307/3065—Flame resistant or retardant, fire resistant or retardant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K2015/03032—Manufacturing of fuel tanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K15/00—Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
- B60K15/03—Fuel tanks
- B60K2015/03032—Manufacturing of fuel tanks
- B60K2015/03046—Manufacturing of fuel tanks made from more than one layer
Definitions
- the present invention relates to nanocomposite vessels for use, e.g. as storage containers for liquids and gasses under high pressure, particularly containers for the storage of compressed natural gas (CNG).
- CNG compressed natural gas
- Pressure vessels are widely used to store liquids and gases under high pressure.
- the storage capacity of a pressure vessel depends on its internal volume and the pressure the vessel is capable of safety containing.
- the size shape and weight of the pressure vessel are often important in a particular application.
- pressure vessels may be used to contain CNG.
- CNG is increasingly viewed as preferable for fueling vehicles.
- One objective of the present invention is to provide polymer nanocomposite containers for storing CNG, and using such containers as a fuel tank on automobiles.
- the application of polymer nanocomposite fuel containers for CNG storage service is governed by both technical and regulatory requirements (Department Of Transportation requirements. DOT Part 571 .304 Standard No. 304 Compressed Nagurl, Gas Fuel Container Integrity), hence another objective of the present invention is to design a nanocomposite vessel such that it is compliant with current regulatory requirements. Current vessels for storing CNG are expensive, are prone to leakage, and may not withstand high pressures.
- the present invention is directed, inter alia, to meeting the above-identified objectives and to overcoming the above- identified drawbacks.
- one embodiment of the invention is a seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material.
- Another embodiment of the invention is seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of: a functionalized thermosetting resin, electrospun epoxy nanocomposite fibers, and a flame resistant agent.
- Yet another embodiment of the invention is seamless nanocomposite tank comprising: a high density polyethylene (HDPE) blow molded into the shape of a gas tank, the gas tank having an inner surface and an outer surface, the inner surface defining a space; the inner surface sputtered with a metal for providing structural integrity, followed by a coating of functionalized epoxy for providing a barrier to hydrocarbons from exiting the tank; and the outer surface embedded with a first outer surface coating of functionalized epoxy followed by a first outer surface layer of electrospun epoxy nanocomposite fibers to provide reinforcement to the tank, followed by a second outer surface coating of functionalized epoxy, followed by a second outer surface layer of electrospun epoxy nanocomposite, followed by a third outer surface coating of functionalized epoxy for providing a barrier to oxygen from entering the tank, followed by a layer of flame resistant foam for providing resistance to wear and damage to the tank and fire.
- HDPE high density polyethylene
- Yet another embodiment of the invention is a method for making a seamless nanocomposite vessel.
- This method comprises: a) forming a vessel from a high density polymer, the vessel having an inner surface and an outer surface, the inner surface defining a space; b) sputtering the inner surface of the vessel with a metal to provide structural integrity to the vessel; c) coating the metal-sputtered inner surface of the vessel with a first functionalized thermosetting resin to provide a barrier for substantially preventing hydrocarbons stored in the space from escaping from the vessel; d) coating the outer surface of the vessel with a second functionalized thermosetting resin; e) coating the outer surface of the vessel after step d with a first electrospun epoxy nanocomposite fiber material to provide further structural support to the vessel; f) coating the electrospun epoxy nanocomposite fiber-embedded outer surface of the vessel with a third functionalized thermosetting resin; g) coating the outer surface of the vessel after step f, with a second electrospun epoxy nanocompo
- Figure 1A shows the structural unit of clay.
- Figure 1 B shows several sheet-like structures stacked together.
- Figure 2A shows an unmodified organoclay.
- Figure 2B shows an organoclay modified with a transition metal ion (TMI), Fe 2+ .
- Figure 3 shows a schematic of a nanocomposite vessel of the present invention. Shown are a vessel (1 ) defining an inner space (5), the wall of the vessel (10) having an inner surface (15) and an outer surface (20).
- a schematic of the cross section of the wall of the vessel (10) shows a first thermosetting resin layer (21 ), a metal layer (25), a high density polymer adapted into the shape of the vessel (30), a second thermosetting resin layer (35), a first thermoplastic material layer (40), a third thermosetting resin layer (45), a second thermoplastic material layer (50), a fourth thermosetting resin layer (55) and a flame resistant layer (60). Also shown is an opening (65) to allow filling of the vessel and discharge of the contents therefrom.
- the weakest point in any composite container is its joint.
- joining systems which, include Butt-and-Wrap, O- Ring, Flush Thread, Flanged, Keyway Joint, Socket Joint (coupled), Threaded and Bonded, Bell and Spigot (matched tapered).
- the strongest joint is a butt-and-wrap joint, but unfortunately this type of joint is both labor and time intensive, requiring multiple applications of resin and reinforcing material with curing time between each application. Coupled joints require gluing or cementing the joints together using couplings made of the same material. This system works well with low-pressure distribution systems, but is generally not used in high pressure applications.
- Clay minerals are the basic component for the preparation of organoclays, the most common type of nanofillers. Essentially clay minerals may be defined as hydrous-layered silicates, which consist of two types of continuous sheetlike structural units.
- One is a tetrahedral sheet of silica, which is arranged as a hexagonal network in which the tips of all the tetrahedral units point in one direction.
- the other structural unit consists of two layers of closely packed oxygen or hydroxyl groups in which aluminum, iron or magnesium atoms are embedded at equidistant from oxygen or hydroxyl as shown in FigurelA.
- Interlayer space or silicate gallery ( Figure 1 B).
- Isomorphic substitution within the layers i.e. of Si by Al or of Si by Mg
- monovalent cations such as Na + ,K + ,Li + residing in the interlayer space.
- cations may be exchanged for other metal or organic cations.
- the ability to exchange cations is an important feature of clay minerals. This can be beneficial in introducing other characteristic via clay modification process.
- one embodiment of the invention is a seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material.
- a "high density polymer” is any polymer which provides the requisite characteristics of the vessel, e.g. strength and heat resistance.
- High density polymers include but are not limited to polyolefins such as polyethylene, polypropylene, polymethylpentene, polybutene-1 and copolymers thereof.
- Other high density polymers include polyamides and polyamide-imides.
- the high density polyamide is high-density polyethylene (HDPE).
- the high density polymer may be adapted into a desired shape by one of many means known to the art. Such means include, but are not limited to blow molding, compression molding, extrusion molding, injection molding and vacuum formation. In some embodiments the high density polymer is adapted into a desired shape by blow molding.
- Another embodiment of the invention is seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of: a functionalized thermosetting resin, electrospun epoxy nanocomposite fibers, and a flame resistant agent.
- thermoplastic material comprise electrospun nanocomposite fibers.
- the electrospun nanocomposite fibers further comprise a filler.
- Such fillers include, but are not limited to a silica, a nanoclay, carbon black, carbon nanotubes, graphite, graphene, fullerenes, carbon onions, aluminum silicate nanotubes, nanocrystalline aluminum alloys reinforced with a ceramic, nanocrystalline semiconductors, cerium oxide nanoparticles, gold nanoparticles, silver nanoparticles, titanium dioxide nanoparticles, palladium nanoparticles, zinc oxide nanoparticles, copper nanoparticles, phosphate nanoparticles, iron-aluminum nanoparticles, calcium phosphate nanoparticles, and combinations thereof.
- Nanoclays include, but are not limited to clays of the montmorillonite, bentonite, kaolinite, hectorite, halloysite and smectite classes. Nanoclayc also include organically modified organoclays. Organoclays can be further modified, e.g. by the introduction of transition metal ions such as iron, nickel, manganese, cobalt, copper, or combinations thereof.
- the filler is selected from the group consisting of nanoclay, carbon black, carbon nanotubes, graphite, graphene, fullerenes, carbon onions, and combinations thereof.
- flame resistant agent is any agent that provides thermal protection. Preferred flame resistant agents provide resistance to wear and damage to the vessel Examples of flame resistant agents include, but are not limited to flame resistant foams.
- Functionalized thermosetting resin include, but are not limited to the group consisting of vinyl ester, epoxy, acrylic, urethane, and combinations thereof. In some embodiments the functionalized thermosetting resin is epoxy.
- thermosetting resin is a resin containing functional groups that improve a desired property, e.g. strength, resistance to heat, resistance to hydrocarbon permeation or resistance to oxygen permeation.
- Functionalized thermosetting resins and methods of their preparation are well known in the art.
- US 20060173142 A1 (Nava and Small)
- U.S. Patent 8,1 19,702 B2 (Luan et al.)
- U.S. patent 5,227,463 A Arsenault
- the functionalized thermosetting resin is functionalized to reduce hydrocarbon permeability.
- the functionalized thermosetting resin is functionalized to reduce hydrocarbon permeability.
- the vessel is selected from the group consisting of a fuel tank, a storage tank, a reaction vessel, a column, a surface condenser, a pressure vessel, and an industrial column.
- the fuel tank is a compressed gas fuel tank.
- the compressed gas fuel tank is a natural gas fuel tank.
- the total number of layers, including the high density polymer is between about 6 to about 12.
- the total number of layers, including the high density polymer is at least 9.
- the vessel has structural properties sufficient to be rated at least FMVSS 304 compliant or a substantial equivalent.
- the vessel has sufficient structural integrity to store a gas at a pressure of at least 4,000 psi.
- Yet another embodiment of the invention is seamless nanocomposite tank comprising: a high density polyethylene (HDPE) blow molded into the shape of a gas tank, the gas tank having an inner surface and an outer surface, the inner surface defining a space; the inner surface sputtered with a metal for providing structural integrity, followed by a coating of functionalized epoxy for providing a barrier to hydrocarbons from exiting the tank; and the outer surface embedded with a first outer surface coating of functionalized epoxy followed by a first outer surface layer of electrospun epoxy nanocomposite fibers to provide reinforcement to the tank, followed by a second outer surface coating of functionalized epoxy, followed by a second outer surface layer of electrospun epoxy nanocomposite, followed by a third outer surface coating of functionalized epoxy for providing a barrier to oxygen from entering the tank, followed by a layer of flame resistant foam for providing resistance to wear and damage to the tank and fire.
- HDPE high density polyethylene
- Yet another embodiment of the invention is a method for making a seamless nanocomposite vessel.
- This method comprises: a) forming a vessel from a high density polymer, the vessel having an inner surface and an outer surface, the inner surface defining a space; b) sputtering the inner surface of the vessel with a metal to provide structural integrity to the vessel; c) coating the metal-sputtered inner surface of the vessel with a first functionalized thermosetting resin to provide a barrier for substantially preventing hydrocarbons stored in the space from escaping from the vessel; d) coating the outer surface of the vessel with a second functionalized thermosetting resin; e) coating the outer surface of the vessel after step d with a first electrospun epoxy nanocomposite fiber material to provide further structural support to the vessel; f) coating the electrospun epoxy nanocomposite fiber-embedded outer surface of the vessel with a third functionalized thermosetting resin; g) coating the outer surface of the vessel after step f, with a second electrospun epoxy nanocompo
- Fuel containers for CNG storage are developed that address each of these issue independently to present a comprehensive solution.
- Polymer nanocomposite fuel tanks primarily are developed using HDPE (high density polyethylene). Physical properties are of key importance in storage tanks developed using polymers. Mechanical properties can be tailored in many ways using various categories of fillers, but barrier properties remain a big challenge. To be an effective barrier, it is necessary not only to maintain its physical integrity when exposed to chemicals, but to also perform as a barrier against these chemicals. Whilst chemical resistance tests provide a measure of resilience, the measure of barrier performance is the permeation rate. This is where HDPE fails as a hydrocarbon resistant barrier because polyethylene and other common homogeneous geo-synthetic membrane materials are readily permeable to hydrocarbons, because they are hydrocarbons themselves.
- Hydrocarbons are non-polar in nature hence there is a need of a polar layer to create an effective barrier for hydrocarbons.
- thermoplastic material is susceptible to a reduction in mechanical properties at elevated temperature, which limits usage of HDPE containers. It is imperative to design multi-component, multilayer polymer nanocomposite materials, which account for enhanced mechanical, reduced barrier and high pressure withholding, properties.
- thermoplastic and thermoset nanocomposite layers are introduced to reinforce the container thus addressing all such issues.
- introduction of fillers in thermoplastic layers enhances the mechanical properties at elevated temperature and provide improved barrier properties.
- Thermosetting resins such as vinyl ester or epoxy can be used to develop layers, which are a part of the container, provide enhanced mechanical properties and have much better resistance to heat.
- Introduction of fillers such as nanoclay further enhances these properties.
- Another layer could be a hybrid layer made up of carbon or glass fibers in the matrix of epoxy resin. This allow for the use of different materials in different layers to design vessels with high barrier and thermal properties and enhanced mechanical strength with high-pressure rating according to the desired end-use.
- Supercritical CO2-processed polymer/clay nanocomposites are developed and characterized for use in natural gas fuel containers.
- a superior quality polymer nanocomposite material which leads to platform technologies for manufacturing economical and high-performance (higher strength and low permeability) natural gas fuel containers with requisite pressure rating is developed.
- Property enhancements in such polymer-nanocomposites are governed by the extent of dispersion of clay particles in the polymer matrix, and the degree of interaction between clay particles and polymer.
- Supercritical CO 2 technology for exfoliation and dispersion of clay is utilized to accomplish this objective.
- This technology creates a strong barrier and strengthens the polymer nanocomposites.
- the fillers processed via supercritical fluid processing technology can be then introduced in a spectrum of polymers (thermoplastic and thermosetting) resins. These fillers have proved to enhance properties without diminishing or altering core polymeric properties. Materials thus produced could be used on existing processing procedures or production lines, and no new setup is required.
- This technology enables controlled placement and dispersion of nanoparticles, which can then be dispersed in a controlled manner within polymer resins. The resulting material has shown drastic improvements in mechanical and permeability properties.
- Scavenging agent and repellants are introduced in clay to enhance the barrier properties of the resulting polymer nanocomposite film.
- a dual barrier is created, which creates a barrier for oxygen to permeate into the containers and stored CNG to escape from the containers.
- Introduction of oxygen scavenging agents on the inside ensure that any oxygen inside is absorbed in the layer and removed from the mix.
- Creating a barrier on the outer surface ensures a barrier against oxygen.
- the inside surface of the container is coated in such a manner that hydrocarbons are repelled and it does not allow hydrocarbons to escape from the container.
- Oxygen scavenging materials are useful in packaging materials, storage containers especially for applications where contamination can result in disaster, providing a longer shelf life to contents.
- metallic scavengers transition metal ions such as Fe, Cu etc.
- the most commonly used oxygen scavengers are based on the principle of iron oxidation.
- the inventors beleive that all the transition metal ions (TMI), which are susceptible to oxidation in the presence of air, can be used as oxygen scavengers.
- TMI especially iron (Fe) and copper (Cu) which show multiple oxidation states
- transition metal ions not only act as oxygen scavengers, but also improve thermal characteristics.
- the compatibility of TMI and polymer matrices is important to consider when using TMI as oxygen scavengers for polymers matrices.
- Organoclays can be made compatible with both transition metal compounds and polymers, and thus can serve as media for the introduction of TMI into polymer matrices. Introducing transition metal ion and reduction of their oxidation state enhances the oxygen scavenging properties of these ions when present in the clay.
- Figures 2A and 2B schematically compare the appearance of an unmodified organoclay to one containing a transition metal compound.
- Hydrocarbons are non-polar in nature hence it is imperative that they do not interact with any non-polar components in the fuel container else permeation will occur.
- the layer interacting with the hydrocarbons can be highly polar in nature coupled with a barrier created by fillers that are introduced in this layer.
- An inner-polar layer, which will protect hydrocarbons from escaping and a non-polar outside layer acting as a barrier against oxygen is therefore desirable.
- Nanocomposite Fuel Tanks [0046] A multilayer, multi-polymer, multi-filler polymer nanocomposite fuel container compliant with Department Of Transportation requirement for storing CNG is developed.
- a multi layer composite material enhances mechanical and barrier properties along with thermal stability.
- Weight is kept at its minimum hence the architecture of multi-component polymer composite is such that weight doesn't increase the current weight of a vehicle.
- a design of a nanocomposite fuel tank according to the present invention which provides mechanical and barrier properties as desired and is able to withhold hydrostatic pressure of 3600 psi or more is developed.
- Design of tank has multiple layers and multiple components and each individual layer has unique characteristics and contributes towards multiple properties. The design can be broken down into individual layers with various characteristics.
- Material of construction is a mix of thermoplastic and thermosetting layers. Each layer is modified using fillers that enhance different properties of the polymer.
- Clay is a sheet like material and it provides tortous path for the any permeating molecule, hence increasing the physical barrier for the permeating molecule. Thermal stability of material increases with the inclusion of clay. Hence inclusion of clay in each individual layer increases thermal stability of that layer and enhances the barrier properties of these layers. Overall, use of clay creates a thermally stable and high barrier multi-layer material for application in fuel tanks.
- Carbon black is a small sheet-like hexagonal nano plate material which forms network points in the polymer matrix and increases the strength of material. Inclusion of carbon black increases the strength of each individual layer, and the over all mechanics of the multilayer material increases.
- Figure 3 shows construction of a nanocomposite vessel of the present invention wherein multiple layers of various resins which contain multiple components are used to achieve desired properties.
- Figure 3 shows a fuel tank (1 ) having the following layers:
- the HDPE nanocomposite layer (30) is a core shell blown molded out of HDPE nanocomposite material.
- HDPE nanocomposite material is developed using HDPE modified with clay and carbon black to provide strength and reduced permeability to the HDPE layer.
- the sputtered metallic coating (25) is present on the inside of the core shell followed by the functionalized epoxy coating (21 ) (innermost layer) which is epoxy modified coating to provide a barrier against hydrocarbon.
- the functionalized epoxy nanocomposite coating (35) is modified epoxy to act as an adhesive layer between HDPE and electrospun fibers.
- the electrospun epoxy nanocomposite fibers (40) are woven to provide strength. Epoxy is modified with fillers like clay, and carbon black to provide enhanced barrier and mechanical properties.
- This epoxy is drawn as an elctrospun fiber and wrapped around the core shell in weaved pattern and then allowed to cure on this surface.
- Adhesive present in the functionalized epoxy nanocomposite coating (35) cure along with this layer such that there is no phase separation.
- the functionalized epoxy nanocomposite coating layer (45) is a modified epoxy to act as an adhesive layer between the two layers of electrospun fibers.
- the electrospun epoxy nanocomposite fibers (50) are woven to provide strength.
- Epoxy is modified with fillers like clay, and carbon black to provide enhanced barrier and mechanical properties. This epoxy is drawn as an elctrospun fiber and wrapped in a weaved pattern.
- the functionalized nanocomposite coating as a barrier against O 2 (55) is the outermost layer of coating which is formulated using modified epoxy such that there is no permeation into the gas tank.
- the protective foam layer (60) is an external sleeve of foam which provides resistance towards damage and fire. It is an impact resistant layer in the tank to minimize damage due to wear and tear.
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Abstract
This invention provides a seamless nanocomposite vessel, which includes a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material. Methods for making and using such vessels also are provided.
Description
NANOCOMPOSITE VESSELS
RELATED APPLICATIONS
[0001] This application claims benefit of U.S. Patent Application Serial No. 61/847,823, filed on July 18, 2013, which application is incorporated by reference herein in its entirety.
FIELD OF THE INVENTION
[0002] The present invention relates to nanocomposite vessels for use, e.g. as storage containers for liquids and gasses under high pressure, particularly containers for the storage of compressed natural gas (CNG).
BACKGROUND OF THE INVENTION
[0003] Pressure vessels are widely used to store liquids and gases under high pressure. The storage capacity of a pressure vessel depends on its internal volume and the pressure the vessel is capable of safety containing. In addition to its storage capacity the size shape and weight of the pressure vessel are often important in a particular application. For example, pressure vessels may be used to contain CNG. CNG is increasingly viewed as preferable for fueling vehicles. There are four types of CNG fuel tanks available in the market today:
1 . Metallic non-composite container;
2. Metallic liner over which an overwrap such as carbon fiber or fiberglass is applied in a hoop wrapped pattern over the liner's cylinder sidewall;
3. Metallic liner over which an overwrap such as carbon fiber or fiberglass is applied in a full wrapped pattern over the entire liner, including the domes; and
4. Non-metallic liner over which an overwrap such as carbon fiber or fiberglass is applied in a full wrapped pattern over the entire liner, including the domes. One objective of the present invention is to provide polymer nanocomposite containers for storing CNG, and using such containers as a fuel tank on automobiles. The application of polymer nanocomposite fuel containers for CNG storage service is governed by both technical and regulatory requirements (Department Of
Transportation requirements. DOT Part 571 .304 Standard No. 304 Compressed Nagurl, Gas Fuel Container Integrity), hence another objective of the present invention is to design a nanocomposite vessel such that it is compliant with current regulatory requirements. Current vessels for storing CNG are expensive, are prone to leakage, and may not withstand high pressures. The present invention is directed, inter alia, to meeting the above-identified objectives and to overcoming the above- identified drawbacks.
SUMMARY OF THE INVENTION
[0004] Thus, one embodiment of the invention is a seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material.
[0005] Another embodiment of the invention is seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of: a functionalized thermosetting resin, electrospun epoxy nanocomposite fibers, and a flame resistant agent.
[0006] Yet another embodiment of the invention is seamless nanocomposite tank comprising: a high density polyethylene (HDPE) blow molded into the shape of a gas tank, the gas tank having an inner surface and an outer surface, the inner surface defining a space; the inner surface sputtered with a metal for providing structural integrity, followed by a coating of functionalized epoxy for providing a barrier to hydrocarbons from exiting the tank; and the outer surface embedded with a first outer surface coating of functionalized epoxy followed by a first outer surface layer of electrospun epoxy nanocomposite fibers to provide reinforcement to the tank, followed by a second outer surface coating of functionalized epoxy, followed by a second outer surface layer of electrospun epoxy nanocomposite, followed by a
third outer surface coating of functionalized epoxy for providing a barrier to oxygen from entering the tank, followed by a layer of flame resistant foam for providing resistance to wear and damage to the tank and fire.
[0007] Yet another embodiment of the invention is a method for making a seamless nanocomposite vessel. This method comprises: a) forming a vessel from a high density polymer, the vessel having an inner surface and an outer surface, the inner surface defining a space; b) sputtering the inner surface of the vessel with a metal to provide structural integrity to the vessel; c) coating the metal-sputtered inner surface of the vessel with a first functionalized thermosetting resin to provide a barrier for substantially preventing hydrocarbons stored in the space from escaping from the vessel; d) coating the outer surface of the vessel with a second functionalized thermosetting resin; e) coating the outer surface of the vessel after step d with a first electrospun epoxy nanocomposite fiber material to provide further structural support to the vessel; f) coating the electrospun epoxy nanocomposite fiber-embedded outer surface of the vessel with a third functionalized thermosetting resin; g) coating the outer surface of the vessel after step f, with a second electrospun epoxy nanocomposite fiber material; h) coating the outer surface of the vessel after step g, with a fourth functionalized thermosetting resin to provide a barrier for substantially preventing oxygen from the outside environment from penetrating into the vessel; and i) applying a flame resistant agent to the outer surface of the vessel after step h, wherein the first, second, third and fourth functionalized thermosetting resin are independently selected and may be the same or different resin.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] The following drawings form part of the present specification and are included to further demonstrate certain aspects of the present invention. The invention may be better understood by reference to one or more of these drawings in combination with the detailed description of specific embodiments presented herein.
[0009] Figure 1A shows the structural unit of clay. Figure 1 B shows several sheet-like structures stacked together.
[0010] Figure 2A shows an unmodified organoclay. Figure 2B shows an organoclay modified with a transition metal ion (TMI), Fe2+.
[0011] Figure 3 shows a schematic of a nanocomposite vessel of the present invention. Shown are a vessel (1 ) defining an inner space (5), the wall of the vessel (10) having an inner surface (15) and an outer surface (20). A schematic of the cross section of the wall of the vessel (10), shows a first thermosetting resin layer (21 ), a metal layer (25), a high density polymer adapted into the shape of the vessel (30), a second thermosetting resin layer (35), a first thermoplastic material layer (40), a third thermosetting resin layer (45), a second thermoplastic material layer (50), a fourth thermosetting resin layer (55) and a flame resistant layer (60). Also shown is an opening (65) to allow filling of the vessel and discharge of the contents therefrom.
DETAILED DESCRIPTION OF THE INVENTION
[0012] While designing polymer-nanocomposite CNG storage containers/fuel tanks, achieving enhanced mechanical and barrier properties is of key importance. Traditionally these fuel tanks were made up of metal, and with the advent of polymer nanocomposite materials, one of the key challenges in developing these storage containers is its ability to withstand high hydrostatic pressure. These containers should be rated equivalent to their metallic counterparts, as the CNG is a pressurized gas stored at a high pressure of 3600 psi.
[0013] The weakest point in any composite container is its joint. Currently there are a number of joining systems available, which, include Butt-and-Wrap, O- Ring, Flush Thread, Flanged, Keyway Joint, Socket Joint (coupled), Threaded and Bonded, Bell and Spigot (matched tapered). The strongest joint is a butt-and-wrap joint, but unfortunately this type of joint is both labor and time intensive, requiring multiple applications of resin and reinforcing material with curing time between each application. Coupled joints require gluing or cementing the joints together using couplings made of the same material. This system works well with low-pressure distribution systems, but is generally not used in high pressure applications. A variation of this is the couple-and-wrap method similar to a butt-and-wrap with a coupling. Threaded FRP pipe with a box and pin configuration is also widely used in oilfield applications. Maintaining a complete seal in natural gas containers at higher pressures however is a challenge with this method of connection. Flanged connection is quick to install, but larger diameters are difficult to work with, and flanged pipe is not cost competitive.
[0014] Clay minerals are the basic component for the preparation of organoclays, the most common type of nanofillers. Essentially clay minerals may be defined as hydrous-layered silicates, which consist of two types of continuous sheetlike structural units. One is a tetrahedral sheet of silica, which is arranged as a hexagonal network in which the tips of all the tetrahedral units point in one direction. The other structural unit (octahedral sheet) consists of two layers of closely packed oxygen or hydroxyl groups in which aluminum, iron or magnesium atoms are embedded at equidistant from oxygen or hydroxyl as shown in FigurelA.
[0015] Stacking of the layers leads to a regular van-der Waals gap between the layers called the interlayer space or silicate gallery (Figure 1 B). Isomorphic substitution within the layers (i.e. of Si by Al or of Si by Mg) generates negative charges at layer surfaces that for some clays may be counterbalanced by monovalent cations such as Na+,K+,Li+ residing in the interlayer space. For certain classes of clays (i.e. smectites) such cations may be exchanged for other metal or organic cations. The ability to exchange cations is an important feature of clay minerals. This can be beneficial in introducing other characteristic via clay modification process.
[0016] In view of the foregoing, the present invention is directed to combining nanocomposite materials and various other layers into a vessel that provides an improved container for CNG, particularly a vessel that may function as a fuel tank for use in the automobile industry. Thus, one embodiment of the invention is a seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material.
[0017] As used herein a "high density polymer" is any polymer which provides the requisite characteristics of the vessel, e.g. strength and heat resistance. High density polymers include but are not limited to polyolefins such as polyethylene, polypropylene, polymethylpentene, polybutene-1 and copolymers thereof. Other high density polymers include polyamides and polyamide-imides. In some embodiments the high density polyamide is high-density polyethylene (HDPE).
[0018] The high density polymer may be adapted into a desired shape by one of many means known to the art. Such means include, but are not limited to blow molding, compression molding, extrusion molding, injection molding and vacuum formation. In some embodiments the high density polymer is adapted into a desired shape by blow molding.
[0019] Another embodiment of the invention is seamless nanocomposite vessel comprising: a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of: a functionalized thermosetting resin, electrospun epoxy nanocomposite fibers, and a flame resistant agent.
[0020] In some embodiments the thermoplastic material comprise electrospun nanocomposite fibers.
[0021] In some embodiments the electrospun nanocomposite fibers further comprise a filler.
[0022] Such fillers include, but are not limited to a silica, a nanoclay, carbon black, carbon nanotubes, graphite, graphene, fullerenes, carbon onions, aluminum silicate nanotubes, nanocrystalline aluminum alloys reinforced with a ceramic, nanocrystalline semiconductors, cerium oxide nanoparticles, gold nanoparticles, silver nanoparticles, titanium dioxide nanoparticles, palladium nanoparticles, zinc oxide nanoparticles, copper nanoparticles, phosphate nanoparticles, iron-aluminum nanoparticles, calcium phosphate nanoparticles, and combinations thereof.
[0023] Nanoclays include, but are not limited to clays of the montmorillonite, bentonite, kaolinite, hectorite, halloysite and smectite classes. Nanoclayc also include organically modified organoclays. Organoclays can be further modified, e.g. by the introduction of transition metal ions such as iron, nickel, manganese, cobalt, copper, or combinations thereof.
[0024] In some embodiments the filler is selected from the group consisting of nanoclay, carbon black, carbon nanotubes, graphite, graphene, fullerenes, carbon onions, and combinations thereof.
[0025] As used herein a "flame resistant agent" is any agent that provides thermal protection. Preferred flame resistant agents provide resistance to wear and
damage to the vessel Examples of flame resistant agents include, but are not limited to flame resistant foams.
[0026] Functionalized thermosetting resin include, but are not limited to the group consisting of vinyl ester, epoxy, acrylic, urethane, and combinations thereof. In some embodiments the functionalized thermosetting resin is epoxy.
[0027] As used herein a "functionalized thermosetting resin" is a resin containing functional groups that improve a desired property, e.g. strength, resistance to heat, resistance to hydrocarbon permeation or resistance to oxygen permeation. Functionalized thermosetting resins and methods of their preparation are well known in the art. For example, US 20060173142 A1 (Nava and Small), U.S. Patent 8,1 19,702 B2 (Luan et al.) and U.S. patent 5,227,463 A (Arsenault), the contents of each of which are incorporated by reference herein in their entireties.
[0028] In some embodiments the functionalized thermosetting resin is functionalized to reduce hydrocarbon permeability.
[0029] In some embodiments the functionalized thermosetting resin is functionalized to reduce hydrocarbon permeability.
[0030] In some embodiments the vessel is selected from the group consisting of a fuel tank, a storage tank, a reaction vessel, a column, a surface condenser, a pressure vessel, and an industrial column. In some embodiments the fuel tank is a compressed gas fuel tank. In some embodiments the compressed gas fuel tank is a natural gas fuel tank.
[0031] In some embodiments the total number of layers, including the high density polymer is between about 6 to about 12.
[0032] In some embodiments the total number of layers, including the high density polymer, is at least 9.
[0033] In some embodiments the vessel has structural properties sufficient to be rated at least FMVSS 304 compliant or a substantial equivalent.
[0034] In some embodiments the vessel has sufficient structural integrity to store a gas at a pressure of at least 4,000 psi.
[0035] Yet another embodiment of the invention is seamless nanocomposite tank comprising: a high density polyethylene (HDPE) blow molded into the shape of a gas tank, the gas tank having an inner surface and an outer surface, the inner surface defining a space; the inner surface sputtered with a metal for providing structural integrity, followed by a coating of functionalized epoxy for providing a
barrier to hydrocarbons from exiting the tank; and the outer surface embedded with a first outer surface coating of functionalized epoxy followed by a first outer surface layer of electrospun epoxy nanocomposite fibers to provide reinforcement to the tank, followed by a second outer surface coating of functionalized epoxy, followed by a second outer surface layer of electrospun epoxy nanocomposite, followed by a third outer surface coating of functionalized epoxy for providing a barrier to oxygen from entering the tank, followed by a layer of flame resistant foam for providing resistance to wear and damage to the tank and fire.
[0036] Yet another embodiment of the invention is a method for making a seamless nanocomposite vessel. This method comprises: a) forming a vessel from a high density polymer, the vessel having an inner surface and an outer surface, the inner surface defining a space; b) sputtering the inner surface of the vessel with a metal to provide structural integrity to the vessel; c) coating the metal-sputtered inner surface of the vessel with a first functionalized thermosetting resin to provide a barrier for substantially preventing hydrocarbons stored in the space from escaping from the vessel; d) coating the outer surface of the vessel with a second functionalized thermosetting resin; e) coating the outer surface of the vessel after step d with a first electrospun epoxy nanocomposite fiber material to provide further structural support to the vessel; f) coating the electrospun epoxy nanocomposite fiber-embedded outer surface of the vessel with a third functionalized thermosetting resin; g) coating the outer surface of the vessel after step f, with a second electrospun epoxy nanocomposite fiber material; h) coating the outer surface of the vessel after step g, with a fourth functionalized thermosetting resin to provide a barrier for substantially preventing oxygen from the outside environment from penetrating into the vessel; and i) applying a flame resistant agent to the outer surface of the vessel after step h, wherein the first, second, third and fourth functionalized thermosetting resin are independently selected and may be the same or different resin.
[0037] The following examples are provided to further illustrate the methods and compositions of the present invention. These examples are illustrative only and are not intended to limit the scope of the invention in any way.
EXAMPLES
EXAMPLE 1
Issues in Storage of Fuel
[0038] There are three main issues in storage of fuel:
1 . Mechanical (including pressure rating) and permeability properties of the fuel container;
2. Weight of the fuel containers; and
3. Cost effectiveness.
[0039] Fuel containers for CNG storage are developed that address each of these issue independently to present a comprehensive solution. Polymer nanocomposite fuel tanks primarily are developed using HDPE (high density polyethylene). Physical properties are of key importance in storage tanks developed using polymers. Mechanical properties can be tailored in many ways using various categories of fillers, but barrier properties remain a big challenge. To be an effective barrier, it is necessary not only to maintain its physical integrity when exposed to chemicals, but to also perform as a barrier against these chemicals. Whilst chemical resistance tests provide a measure of resilience, the measure of barrier performance is the permeation rate. This is where HDPE fails as a hydrocarbon resistant barrier because polyethylene and other common homogeneous geo-synthetic membrane materials are readily permeable to hydrocarbons, because they are hydrocarbons themselves. Hydrocarbons are non-polar in nature hence there is a need of a polar layer to create an effective barrier for hydrocarbons. Also, thermoplastic material is susceptible to a reduction in mechanical properties at elevated temperature, which limits usage of HDPE containers. It is imperative to design multi-component, multilayer polymer nanocomposite materials, which account for enhanced mechanical, reduced barrier and high pressure withholding, properties.
[0040] A combination of thermoplastic and thermoset nanocomposite layers is introduced to reinforce the container thus addressing all such issues. In addition, introduction of fillers in thermoplastic layers enhances the mechanical properties at elevated temperature and provide improved barrier properties. Thermosetting resins, such as vinyl ester or epoxy can be used to develop layers, which are a part of the container, provide enhanced mechanical properties and have much better resistance to heat. Introduction of fillers such as nanoclay, further enhances these properties. Another layer could be a hybrid layer made up of carbon or glass fibers in the matrix
of epoxy resin. This allow for the use of different materials in different layers to design vessels with high barrier and thermal properties and enhanced mechanical strength with high-pressure rating according to the desired end-use.
EXAMPLE 2
Nanocomposite Technology
[0041] Supercritical CO2-processed polymer/clay nanocomposites are developed and characterized for use in natural gas fuel containers. A superior quality polymer nanocomposite material, which leads to platform technologies for manufacturing economical and high-performance (higher strength and low permeability) natural gas fuel containers with requisite pressure rating is developed. Property enhancements in such polymer-nanocomposites are governed by the extent of dispersion of clay particles in the polymer matrix, and the degree of interaction between clay particles and polymer. Supercritical CO2 technology for exfoliation and dispersion of clay is utilized to accomplish this objective.
[0042] This technology creates a strong barrier and strengthens the polymer nanocomposites. The fillers processed via supercritical fluid processing technology can be then introduced in a spectrum of polymers (thermoplastic and thermosetting) resins. These fillers have proved to enhance properties without diminishing or altering core polymeric properties. Materials thus produced could be used on existing processing procedures or production lines, and no new setup is required. This technology enables controlled placement and dispersion of nanoparticles, which can then be dispersed in a controlled manner within polymer resins. The resulting material has shown drastic improvements in mechanical and permeability properties.
EXAMPLE 3
Polymer Layer Modification Using Scavengers and Repellants
[0043] Scavenging agent and repellants are introduced in clay to enhance the barrier properties of the resulting polymer nanocomposite film. For containers containing CNG gas it is imperative that a dual barrier is created, which creates a barrier for oxygen to permeate into the containers and stored CNG to escape from the containers. Introduction of oxygen scavenging agents on the inside ensure that any oxygen inside is absorbed in the layer and removed from the mix. Creating a barrier on the outer surface ensures a barrier against oxygen. The inside surface of
the container is coated in such a manner that hydrocarbons are repelled and it does not allow hydrocarbons to escape from the container.
[0044] Oxygen scavenging materials are useful in packaging materials, storage containers especially for applications where contamination can result in disaster, providing a longer shelf life to contents. In industry using metallic scavengers (transition metal ions such as Fe, Cu etc.) is common practice and they are used in the form of powder packed in a sachet, which is inserted in the product. The most commonly used oxygen scavengers are based on the principle of iron oxidation. Not wishing to be bound to a particular theory, the inventors beleive that all the transition metal ions (TMI), which are susceptible to oxidation in the presence of air, can be used as oxygen scavengers. TMI especially iron (Fe) and copper (Cu) which show multiple oxidation states, are of great interest due to their catalytic activity for specific reactions such as hydrosilylation, oxidation, C-C coupling, and selective hydrogenation. Such transition metal ions not only act as oxygen scavengers, but also improve thermal characteristics. The compatibility of TMI and polymer matrices is important to consider when using TMI as oxygen scavengers for polymers matrices. Organoclays can be made compatible with both transition metal compounds and polymers, and thus can serve as media for the introduction of TMI into polymer matrices. Introducing transition metal ion and reduction of their oxidation state enhances the oxygen scavenging properties of these ions when present in the clay. Figures 2A and 2B schematically compare the appearance of an unmodified organoclay to one containing a transition metal compound.
[0045] Hydrocarbons are non-polar in nature hence it is imperative that they do not interact with any non-polar components in the fuel container else permeation will occur. To be able to create a high-barrier for hydrocarbons, the layer interacting with the hydrocarbons can be highly polar in nature coupled with a barrier created by fillers that are introduced in this layer. An inner-polar layer, which will protect hydrocarbons from escaping and a non-polar outside layer acting as a barrier against oxygen is therefore desirable.
EXAMPLE 4
Nanocomposite Fuel Tanks
[0046] A multilayer, multi-polymer, multi-filler polymer nanocomposite fuel container compliant with Department Of Transportation requirement for storing CNG is developed.
1 . A multi layer composite material enhances mechanical and barrier properties along with thermal stability.
2. Selection of material is strictly based on pressure rating, as for storing CNG a container must be able to withhold 3600 or more psi.
3. Weight is kept at its minimum hence the architecture of multi-component polymer composite is such that weight doesn't increase the current weight of a vehicle.
EXAMPLE 5
Prototype Fuel Tank
[0047] A design of a nanocomposite fuel tank according to the present invention, which provides mechanical and barrier properties as desired and is able to withhold hydrostatic pressure of 3600 psi or more is developed. Design of tank has multiple layers and multiple components and each individual layer has unique characteristics and contributes towards multiple properties. The design can be broken down into individual layers with various characteristics.
[0048] Material of construction is a mix of thermoplastic and thermosetting layers. Each layer is modified using fillers that enhance different properties of the polymer. Clay is a sheet like material and it provides tortous path for the any permeating molecule, hence increasing the physical barrier for the permeating molecule. Thermal stability of material increases with the inclusion of clay. Hence inclusion of clay in each individual layer increases thermal stability of that layer and enhances the barrier properties of these layers. Overall, use of clay creates a thermally stable and high barrier multi-layer material for application in fuel tanks. Carbon black is a small sheet-like hexagonal nano plate material which forms network points in the polymer matrix and increases the strength of material. Inclusion of carbon black increases the strength of each individual layer, and the over all mechanics of the multilayer material increases. These are low cost additives and are used to enhance the mechanical, thermal and barrier properties of material for storing CNG. Surface modification of epoxy with, e.g., florination or sulfonation, provides a chemical barrier by repelling action and hence improves specific barrier
properties of these layers. The inside layers may be coated with modified epoxy such that hydrocarbons cannot escape. Also, the metallic layer provides a strong barrier for permeating hydrocarbon molecules, if any. This eliminates the possibility of leaks in the fuel tank.
[0049] In a composite fuel tank there are usually two stresses that can develop one along the circumference and other along the tangential axis. Wrapping of epoxy nanocomposite fibers takes care of such stresses and provide requisite strength to the core shell. Conventionally carbon fibers have been used to provide this strength; here a similar strength is achieved using epoxy nanocomposite fibers. An outermost layer of foam provides impact resistance to the gas tank and will protect from regular wear tare. This protective foam can be flame retardant hence protecting the contents of tank in an event of fire.
[0050] In this design the approximate dimensions of the CNG fuel tank are:
Length 55 to 56 inches
Diameter 16 inches
Weight 45 to 50 kgs
Thickness of walls 2"
Volume of water 130L
[0051] This is illustrated in Figure 3, which shows construction of a nanocomposite vessel of the present invention wherein multiple layers of various resins which contain multiple components are used to achieve desired properties.
[0052] In particular, Figure 3 shows a fuel tank (1 ) having the following layers:
a) A functionalized epoxy coating (21 );
b) A sputtered metallic coating (25);
c) A HDPE nanocomposite layer (30);
d) A functionalized epoxy nanocomposite coating (35); e) Electrospun epoxy nanocomposite fibers (40);
f) A functionalized epoxy nanocomposite coating (45); g) Electrospun epoxy nanocomposite fibers (50);
h) A functionalized nanocomposite coating as a barrier against O2 (45); and
i) A protective foam layer.
[0053] The HDPE nanocomposite layer (30) is a core shell blown molded out of HDPE nanocomposite material. HDPE nanocomposite material is developed using
HDPE modified with clay and carbon black to provide strength and reduced permeability to the HDPE layer. The sputtered metallic coating (25) is present on the inside of the core shell followed by the functionalized epoxy coating (21 ) (innermost layer) which is epoxy modified coating to provide a barrier against hydrocarbon. The functionalized epoxy nanocomposite coating (35) is modified epoxy to act as an adhesive layer between HDPE and electrospun fibers. The electrospun epoxy nanocomposite fibers (40) are woven to provide strength. Epoxy is modified with fillers like clay, and carbon black to provide enhanced barrier and mechanical properties. This epoxy is drawn as an elctrospun fiber and wrapped around the core shell in weaved pattern and then allowed to cure on this surface. Adhesive present in the functionalized epoxy nanocomposite coating (35) cure along with this layer such that there is no phase separation. The functionalized epoxy nanocomposite coating layer (45) is a modified epoxy to act as an adhesive layer between the two layers of electrospun fibers. The electrospun epoxy nanocomposite fibers (50) are woven to provide strength. Epoxy is modified with fillers like clay, and carbon black to provide enhanced barrier and mechanical properties. This epoxy is drawn as an elctrospun fiber and wrapped in a weaved pattern. The functionalized nanocomposite coating as a barrier against O2 (55) is the outermost layer of coating which is formulated using modified epoxy such that there is no permeation into the gas tank. The protective foam layer (60) is an external sleeve of foam which provides resistance towards damage and fire. It is an impact resistant layer in the tank to minimize damage due to wear and tear.
[0054] Although illustrative embodiments of the present invention have been described herein, it should be understood that the invention is not limited to those described, and that various other changes or modifications may be made by one skilled in the art without departing from the scope or spirit of the invention.
Claims
1 . A seamless nanocomposite vessel comprising:
(a) a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space; and
(b) a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of a thermoplastic material and a thermoset nanocomposite material.
2. A seamless nanocomposite vessel comprising:
(a) a high density polymer adapted into the shape of a desired vessel, the vessel having an inner surface sputtered with a metal and an outer surface, the inner surface defining a space;
(b) a plurality of layers disposed over the inner surface of the vessel, the outer surface of the vessel, or both, each layer being independently selected from the group consisting of: a functionalized thermosetting resin, electrospun epoxy nanocomposite fibers, and a flame resistant agent.
3. The seamless nanocomposite vessel according to claim 2 in which the electrospun nanocomposite fibers further comprise a filler.
4. The seamless nanocomposite vessel according to claim 3, wherein the filler is selected from the group consisting of nanoclay, carbon black, carbon nanotubes, graphite, graphene, fullerenes, carbon onions, and combinations thereof.
5. The seamless nanocomposite vessel according to claim 2, wherein the flame resistant agent is a flame resistant foam.
6. The seamless nanocomposite vessel according to claim 2, wherein the functionalized thermosetting resin is selected from the group consisting of vinyl ester, epoxy, acrylic and urethane.
7. The seamless nanocomposite vessel according to claim 6, wherein the functionalized thermosetting resin is epoxy.
8. The seamless nanocomposite vessel according to claim 2, wherein the functionalized thermosetting resin is functionalized to reduce hydrocarbon permeability.
9. The seamless nanocomposite vessel according to claim 2, wherein the functionalized thermosetting resin is functionalized to reduce oxygen permeability.
10. The seamless nanocomposite vessel according to claim 2, wherein the high density polymer is selected from the group consisting of high density polyethylene (HDPE), polypropylene, polymethylpentene, polybutene-1 polyamides polyamide-imides and combinationa thereof.
1 1 . The seamless nanocomposite vessel according to claim 2, wherein the high density polymer is HDPE.
12. The seamless nanocomposite vessel according to claim 2, wherein the vessel is selected from the group consisting of a fuel tank, a storage tank, a reaction vessel, a column, a surface condenser, a pressure vessel, and an industrial column.
13. The seamless nanocomposite vessel according to claim 12, wherein the fuel tank is a compressed gas fuel tank.
14. The seamless nanocomposite vessel according to claim 13, wherein the compressed gas fuel tank is a compressed natural gas fuel tank.
15. The seamless nanocomposite vessel according to claim 2, wherein the total number of layers, including the high density polymer is between about 6 to about 12.
16. The seamless nanocomposite vessel according to claim 14, wherein the total number of layers, including the high density polymer, is at least 9.
17. The seamless nanocomposite vessel according to claim 2, which has structural properties sufficient to be rated at least FMVSS 304 compliant.
18. The seamless nanocomposite vessel according to claim 2, which has sufficient structural integrity to store a gas at a pressure of at least 4,000 psi.
19. A seamless nanocomposite tank comprising:
(a) a high density polyethylene (HDPE) blow molded into the shape of a gas tank, the gas tank having an inner surface and an outer surface, the inner surface defining a space;
i. the inner surface sputtered with a metal for providing structural integrity, followed by a coating of functionalized epoxy for providing a barrier to hydrocarbons from exiting the tank; and ii. the outer surface embedded with a first outer surface coating of functionalized epoxy followed by a first outer surface layer of electrospun epoxy nanocomposite fibers to provide reinforcement to the tank, followed by a second outer surface coating of functionalized epoxy, followed by a second outer surface layer of electrospun epoxy nanocomposite, followed by a third outer surface coating of functionalized epoxy for providing a barrier to oxygen from entering the tank, followed by
a layer of flame resistant foam for providing resistance to wear and damage to the tank and fire.
20. A method for making a seamless nanocomposite vessel comprising:
a. forming a vessel from a high density polymer, the vessel having an inner surface and an outer surface, the inner surface defining a space; b. sputtering the inner surface of the vessel with a metal to provide structural integrity to the vessel;
c. coating the metal-sputtered inner surface of the vessel with a first functionalized thermosetting resin to provide a barrier for substantially preventing hydrocarbons stored in the space from escaping from the vessel;
d. coating the outer surface of the vessel with a second functionalized thermosetting resin;
e. coating the outer surface of the vessel after step d with a first electrospun epoxy nanocomposite fiber material to provide further structural support to the vessel;
f. coating the electrospun epoxy nanocomposite fiber-embedded outer surface of the vessel with a third functionalized thermosetting resin;
g. coating the outer surface of the vessel after step f, with a second electrospun epoxy nanocomposite fiber material;
h. coating the outer surface of the vessel after step g, with a fourth functionalized thermosetting resin to provide a barrier for substantially preventing oxygen from the outside environment from penetrating into the vessel; and
i. applying a flame resistant agent to the outer surface of the vessel after step h,
wherein the first, second, third and fourth functionalized thermosetting resin are independently selected and may be the same or different resin.
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US201361847823P | 2013-07-18 | 2013-07-18 | |
PCT/US2014/047300 WO2015010090A2 (en) | 2013-07-18 | 2014-07-18 | Nanocomposite vessels |
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DE102015208511A1 (en) * | 2015-05-07 | 2016-11-10 | Bayerische Motoren Werke Aktiengesellschaft | Method for preventing the evaporation of fuel and corresponding fuel tank of a motor vehicle |
DE102022105276A1 (en) | 2022-03-07 | 2023-09-07 | Knorr-Bremse Gesellschaft Mit Beschränkter Haftung | METHOD OF MAKING A FIRE RETARDANT CASE, FIRE RETARDANT CASE AND SYSTEM WITH A FIRE RETARDANT CASE |
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US8349986B2 (en) * | 2004-09-01 | 2013-01-08 | Ppg Industries Ohio, Inc. | Poly(ureaurethane)s, articles and coatings prepared therefrom and methods of making the same |
US7700167B2 (en) * | 2006-08-31 | 2010-04-20 | Honeywell International Inc. | Erosion-protective coatings on polymer-matrix composites and components incorporating such coated composites |
US8597747B2 (en) * | 2006-12-15 | 2013-12-03 | Centro, Inc. | Multi-layer rotationally molded low permeation vessels and method for manufacture therof |
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